長パルス1次レーダーによるUSERS REVカプセルの追跡

Material type: 文書・図像類

Author: 鎌田, 幸男ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2005-03-31

Material Format: Digital

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Note (General)：: After 8.5 month-experiments in orbit, the Recovery Vehicle (REV) of the USERS satellite was reentered into the atmosphere and successfully retrieved o...

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Material Type: 文書・図像類
Title: 長パルス1次レーダーによるUSERS REVカプセルの追跡
Author/Editor: 鎌田, 幸男
川原, 康介
佐川, 一美
石井, 信明
前田, 行雄
井上, 浩三郎
安部, 隆士
若林, 昭
伊地智, 幸一
Kamata, Yukio
Kawahara, Kosuke
Sagawa, Kazumi
Ishii, Nobuaki
Maeda, Yukio
Inoue, Kozaburo
Abe, Takashi
Wakabayashi, Akira
Ijichi, Koichi
Author Heading: 鎌田, 幸男
川原, 康介
佐川, 一美
石井, 信明
前田, 行雄
井上, 浩三郎
安部, 隆士
若林, 昭
伊地智, 幸一
Kamata, Yukio
Kawahara, Kosuke
Sagawa, Kazumi
Ishii, Nobuaki
Maeda, Yukio
Inoue, Kozaburo
Abe, Takashi
Wakabayashi, Akira
Ijichi, Koichi
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2005-03-31
Publication Date (W3CDTF): 2005-03-31
Alternative Title: Orbit tracking of USERS Recovery Vehicle (REV) with a high performance long pulse primary radar
Periodical title: 宇宙航空研究開発機構研究開発報告: USERS REVカプセルの開発研究および飛行後解析 = JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis
No. or year of volume/issue: JAXA-RR-04-045
Volume: JAXA-RR-04-045
Pages: 105-111
ISSN (Periodical Title): ISSN : 1349-1113
Text Language Code: jpn
Subject Heading: USERSミッション
宇宙機再突入
リエントリモジュール
長パルス1次レーダ
回収機
再突入飛跡
追尾アンテナ
USERS mission
spacecraft reentry
reentry module
long pulse primary radar
recovery vehicle
reentry trajectory
tracking antenna
Target Audience: 一般
Note (General): After 8.5 month-experiments in orbit, the Recovery Vehicle (REV) of the USERS satellite was reentered into the atmosphere and successfully retrieved on the sea in May 30th, 2003. During the atmospheric flight, the trajectory of the vehicle was tracked with the new precision radar system at Kagoshima Space Center, Uchinoura, Kagoshima. Since, the vehicle has no active tracking instrument such as transponder, the primary radar should be utilized so as to detect the object. However, the usual primary radar system is insufficient to track the tiny vehicle. Thus, a high performance long-pulse primary radar, which had capability of recognizing the 1 sq m object at the distant of approximately 2,000 km range, was applied to the tracking operation. Initially, the radar caught the reentry vehicle in the previously predicted direction. However, the radar lost the tracking data, intermediately. In this paper, the operation sequence of the reentry tracking is briefly introduced. Then, the tracking result is summarized with the estimation of the impact point by the off-line computation.
資料番号: AA0048710007
レポート番号: JAXA-RR-04-045
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2323&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2323&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ